BRPI0414047A - nested hitch impulse inverter - Google Patents
nested hitch impulse inverterInfo
- Publication number
- BRPI0414047A BRPI0414047A BRPI0414047-8A BRPI0414047A BRPI0414047A BR PI0414047 A BRPI0414047 A BR PI0414047A BR PI0414047 A BRPI0414047 A BR PI0414047A BR PI0414047 A BRPI0414047 A BR PI0414047A
- Authority
- BR
- Brazil
- Prior art keywords
- hook
- inverter
- nested
- impulse
- pin
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
- F02K1/766—Control or regulation of thrust reversers with blocking systems or locking devices; Arrangement of locking devices for thrust reversers
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B47/00—Operating or controlling locks or other fastening devices by electric or magnetic means
- E05B47/06—Controlling mechanically-operated bolts by electro-magnetically-operated detents
- E05B47/0607—Controlling mechanically-operated bolts by electro-magnetically-operated detents the detent moving pivotally or rotatively
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05C—BOLTS OR FASTENING DEVICES FOR WINGS, SPECIALLY FOR DOORS OR WINDOWS
- E05C3/00—Fastening devices with bolts moving pivotally or rotatively
- E05C3/02—Fastening devices with bolts moving pivotally or rotatively without latching action
- E05C3/06—Fastening devices with bolts moving pivotally or rotatively without latching action with operating handle or equivalent member moving otherwise than rigidly with the bolt
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/64—Reversing fan flow
- F02K1/70—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing
- F02K1/72—Reversing fan flow using thrust reverser flaps or doors mounted on the fan housing the aft end of the fan housing being movable to uncover openings in the fan housing for the reversed flow
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/54—Nozzles having means for reversing jet thrust
- F02K1/76—Control or regulation of thrust reversers
- F02K1/763—Control or regulation of thrust reversers with actuating systems or actuating devices; Arrangement of actuators for thrust reversers
-
- E—FIXED CONSTRUCTIONS
- E05—LOCKS; KEYS; WINDOW OR DOOR FITTINGS; SAFES
- E05B—LOCKS; ACCESSORIES THEREFOR; HANDCUFFS
- E05B53/00—Operation or control of locks by mechanical transmissions, e.g. from a distance
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
"INVERSOR DE IMPULSO DE ENGATE ANINHADO". Um inversor de impulso (36) inclui portas inversoras (54) montadas de maneira articulada em uma nacela (16). Cada porta (54) inclui um pino de engate (70) montado na extremidade distal dela. Um gancho de engate complementar (2) é montado de maneira articulada na nacela (16) para contato com o pino (70) de modo a fechar por engatamento a porta inversora (54) . Um retentor giratório (74) fica contíguo ao gancho (72) para bloquear a rotação do gancho de modo a fechar por engate a porta (54) e desbloquear seletivamente a rotação do gancho (72) para permitir que o pino (70) se desengate do gancho."Nested Impulse Impulse Inverter". A pulse inverter (36) includes hingedly mounted inverter doors (54) in a nacelle (16). Each port (54) includes a snap pin (70) mounted at the distal end thereof. A complementary coupling hook (2) is pivotally mounted to the nacelle (16) for contact with pin (70) to engage the reversing door (54) by engaging. A swivel retainer (74) adjoins the hook (72) to lock the rotation of the hook to lock the door (54) and selectively unlock the rotation of the hook (72) to allow the pin (70) to disengage. of the hook.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US50076703P | 2003-09-05 | 2003-09-05 | |
PCT/US2004/028255 WO2005040589A2 (en) | 2003-09-05 | 2004-08-31 | Nested latch thrust reverser |
Publications (2)
Publication Number | Publication Date |
---|---|
BRPI0414047A true BRPI0414047A (en) | 2006-10-24 |
BRPI0414047B1 BRPI0414047B1 (en) | 2019-08-27 |
Family
ID=34519985
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0414047A BRPI0414047B1 (en) | 2003-09-05 | 2004-08-31 | impulse inverter |
Country Status (5)
Country | Link |
---|---|
US (1) | US7146796B2 (en) |
EP (1) | EP1676025B1 (en) |
BR (1) | BRPI0414047B1 (en) |
CA (1) | CA2536693C (en) |
WO (1) | WO2005040589A2 (en) |
Families Citing this family (53)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7264203B2 (en) * | 2003-10-02 | 2007-09-04 | The Nordam Group, Inc. | Spider actuated thrust reverser |
GB0505612D0 (en) * | 2005-03-21 | 2005-04-27 | Goodrich Actuation Systems Ltd | Lock arrangement |
US8015797B2 (en) | 2006-09-21 | 2011-09-13 | Jean-Pierre Lair | Thrust reverser nozzle for a turbofan gas turbine engine |
FR2908109B1 (en) * | 2006-11-03 | 2008-12-12 | Aircelle Sa | TURBOREACTOR NACELLE ELEMENT |
FR2914956A1 (en) * | 2007-04-12 | 2008-10-17 | Aircelle Sa | NACELLE FOR TURBOJET ENGINEER EQUIPPED WITH A FORWARD REVERSAL SYSTEM |
CN101939528B (en) * | 2007-08-08 | 2013-07-24 | 罗尔股份有限公司 | Variable area fan nozzle with bypass flow |
US9759087B2 (en) | 2007-08-08 | 2017-09-12 | Rohr, Inc. | Translating variable area fan nozzle providing an upstream bypass flow exit |
FR2920140B1 (en) * | 2007-08-20 | 2009-10-30 | Aircelle Sa | NACELLE DE TURBOREACTEUR, INTENDED TO EQUIP AN AIRCRAFT |
FR2922958B1 (en) * | 2007-10-25 | 2009-11-20 | Aircelle Sa | THRUST INVERTER WITH GRILLS |
US7735778B2 (en) * | 2007-11-16 | 2010-06-15 | Pratt & Whitney Canada Corp. | Pivoting fairings for a thrust reverser |
US8172175B2 (en) | 2007-11-16 | 2012-05-08 | The Nordam Group, Inc. | Pivoting door thrust reverser for a turbofan gas turbine engine |
US8091827B2 (en) | 2007-11-16 | 2012-01-10 | The Nordam Group, Inc. | Thrust reverser door |
US8052085B2 (en) | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser for a turbofan gas turbine engine |
US8052086B2 (en) | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser door |
US8002217B2 (en) * | 2007-11-16 | 2011-08-23 | Spirit Aerosystems, Inc. | System for adjustment of thrust reverser pivot door |
US8051639B2 (en) | 2007-11-16 | 2011-11-08 | The Nordam Group, Inc. | Thrust reverser |
US7762086B2 (en) * | 2008-03-12 | 2010-07-27 | United Technologies Corporation | Nozzle extension assembly for ground and flight testing |
FR2929998B1 (en) * | 2008-04-14 | 2011-08-12 | Aircelle Sa | DOUBLE FLOW TURBOREACTOR NACELLE |
GB2460088B (en) * | 2008-05-16 | 2012-05-09 | Ge Aviat Systems Ltd | Locking assembly |
US8127530B2 (en) | 2008-06-19 | 2012-03-06 | The Nordam Group, Inc. | Thrust reverser for a turbofan gas turbine engine |
FR2933143B1 (en) * | 2008-06-26 | 2011-06-10 | Airbus France | NACELLE FOR AN AIRCRAFT COMPRISING INVERTER PUSHING MEANS AND AIRCRAFT COMPRISING AT LEAST ONE SUCH NACELLE |
US8869507B2 (en) * | 2010-01-13 | 2014-10-28 | United Technologies Corporation | Translatable cascade thrust reverser |
US8713911B2 (en) | 2010-12-15 | 2014-05-06 | Woodward Hrt, Inc. | System and method for operating a thrust reverser for a turbofan propulsion system |
FR2970521B1 (en) * | 2011-01-17 | 2013-01-04 | Aircelle Sa | THRUST INVERTER FOR AN AIRCRAFT AIRCRAFT WITH LOW NUMBER OF LATCHES |
US20130042630A1 (en) * | 2011-08-19 | 2013-02-21 | United Technologies Corporation | Gas turbine engine accessory mount |
FR2982324B1 (en) * | 2011-11-09 | 2013-11-15 | Aircelle Sa | PUSH-IN REVERSER WITH TWIN DOORS |
US9109462B2 (en) * | 2011-12-15 | 2015-08-18 | United Technologies Corporation | Energy-absorbing fan case for a gas turbine engine |
US9255546B2 (en) * | 2012-02-02 | 2016-02-09 | Spirit AreoSystems, Inc. | Cascade-style variable area fan duct nozzle |
WO2014092757A1 (en) * | 2012-12-11 | 2014-06-19 | United Technologies Corporation | Asymmetric thrust reversers |
US10060292B2 (en) | 2013-03-14 | 2018-08-28 | United Technologies Corporation | Castellated latch mechanism for a gas turbine engine |
US10077739B2 (en) * | 2014-04-24 | 2018-09-18 | Rohr, Inc. | Dual actuation system for cascade and thrust reverser panel for an integral cascade variable area fan nozzle |
US10487690B2 (en) * | 2014-08-18 | 2019-11-26 | Rohr, Inc. | Actively controlled cooling air exhaust door on an aircraft engine nacelle |
US10309343B2 (en) * | 2014-11-06 | 2019-06-04 | Rohr, Inc. | Split sleeve hidden door thrust reverser |
US9945324B2 (en) | 2014-11-06 | 2018-04-17 | Rohr, Inc. | Sleeve linkage for thrust reverser |
US10208708B2 (en) | 2015-01-29 | 2019-02-19 | Rohr, Inc. | Translating cascade hidden blocker door thrust reverser |
US9689345B2 (en) | 2015-06-10 | 2017-06-27 | Woodward, Inc. | Electric track lock |
US10077740B2 (en) * | 2015-10-16 | 2018-09-18 | The Boeing Company | Folding door thrust reversers for aircraft engines |
EP3168138B1 (en) * | 2015-11-10 | 2018-06-06 | Airbus Operations GmbH | Aircraft door assembly |
US10138843B2 (en) | 2015-11-16 | 2018-11-27 | Rohr, Inc. | Drag link assembly for a thrust reverser |
US10473057B2 (en) | 2015-12-14 | 2019-11-12 | Rohr, Inc. | Thrust reverser system with translating elements |
US10563615B2 (en) * | 2016-05-09 | 2020-02-18 | Mra Systems, Llc | Gas turbine engine with thrust reverser assembly and method of operating |
US9976696B2 (en) | 2016-06-21 | 2018-05-22 | Rohr, Inc. | Linear actuator with multi-degree of freedom mounting structure |
CN108661821B (en) * | 2017-03-31 | 2022-03-18 | Mra系统有限责任公司 | Thrust reverser assembly and method of operation |
US10618664B2 (en) * | 2017-06-16 | 2020-04-14 | Rohr, Inc. | Self-latching nacelle |
EP3428435B1 (en) | 2017-07-13 | 2019-12-11 | Goodrich Actuation Systems Limited | Actuator for use in aircraft |
US10612491B2 (en) * | 2017-09-25 | 2020-04-07 | Rohr, Inc. | Mounting device with pin actuator |
US10731738B2 (en) | 2017-11-27 | 2020-08-04 | Rohr, Inc. | Kinematic system with motion control device |
US10780987B2 (en) | 2018-04-03 | 2020-09-22 | Rohr, Inc. | Fan cowl latch concept for fuselage mounted power plant |
US11441514B2 (en) | 2018-10-02 | 2022-09-13 | Woodward, Inc. | Tertiary lock |
US10865738B2 (en) | 2019-02-27 | 2020-12-15 | Woodward, Inc. | Traveling finger lock for an actuator |
KR20220091174A (en) * | 2020-12-23 | 2022-06-30 | 한화에어로스페이스 주식회사 | Intake opening device for ramjet engine |
US11788490B1 (en) | 2022-12-05 | 2023-10-17 | Woodward, Inc. | Traveling finger lock for an actuator |
US11891964B1 (en) | 2023-08-14 | 2024-02-06 | Rolls-Royce North American Technologies Inc. | Method of manufacture of plug nozzle with thrust reverser |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3503211A (en) | 1968-04-10 | 1970-03-31 | Rohr Corp | Thrust reverser |
US3614037A (en) | 1969-09-22 | 1971-10-19 | Boeing Co | Aircraft combination thrust reverser and sound suppressor and a particular full range balanced thrust reverser |
US3779010A (en) | 1972-08-17 | 1973-12-18 | Gen Electric | Combined thrust reversing and throat varying mechanism for a gas turbine engine |
US3829020A (en) | 1973-06-13 | 1974-08-13 | Boeing Co | Translating sleeve variable area nozzle and thrust reverser |
GB2154291B (en) | 1984-02-14 | 1987-08-12 | Rolls Royce | Anti rotation device |
FR2622929A1 (en) | 1987-11-05 | 1989-05-12 | Hispano Suiza Sa | DRIVE INVERTER OF GRID TURBOREACTOR, WITH VARIABLE EJECTION SECTION |
US5224342A (en) * | 1992-02-13 | 1993-07-06 | Lair Jean Pierre | Latching and sealing arrangement for jet engine thrust reverser |
GB9215496D0 (en) * | 1992-07-21 | 1992-09-02 | Lucas Ind Plc | Lock for an engine thrust reverser |
GB9320447D0 (en) * | 1993-10-05 | 1993-12-22 | Lucas Ind Plc | Lock for an engine thrust reverser |
FR2711187B1 (en) * | 1993-10-15 | 1996-02-02 | Aerospatiale | Double-flow turbojet engine surrounded by a force recovery belt linked to at least one pivoting door of the thrust reversers. |
US5720449A (en) * | 1993-11-19 | 1998-02-24 | Societe De Construction Des Avions Hurel-Dubois | Thrust reverser with doors for aircraft engine, equipped with safety systems preventing the untimely opening of the doors |
GB9418895D0 (en) * | 1994-09-20 | 1994-11-09 | Lucas Ind Plc | Lock mechanism |
FR2727468B1 (en) | 1994-11-30 | 1996-12-27 | Hispano Suiza Sa | DOWNSTREAM OBSTACLE TURBOREACTOR DRIVER |
US5655360A (en) | 1995-05-31 | 1997-08-12 | General Electric Company | Thrust reverser with variable nozzle |
FR2741910B1 (en) | 1995-11-30 | 1998-01-02 | Hispano Suiza Sa | DOOR REVERSER OF TURBOJET WITH DOORS WITH ARTICULATED REAR PANEL |
US5826823A (en) | 1996-02-07 | 1998-10-27 | Rohr, Inc. | Actuator and safety lock system for pivoting door thrust reverser for aircraft jet engine |
FR2745035B1 (en) * | 1996-02-15 | 1998-04-03 | Hispano Suiza Sa | TURBOREACTOR DRIVE INVERTER WITH DOORS ASSOCIATED WITH A UPSTREAM PANEL |
FR2754314B1 (en) * | 1996-10-03 | 1999-01-08 | Hispano Suiza Sa | METHOD AND DEVICES FOR CLOSING THE DOORS OF PUSH INVERTERS |
FR2761734B1 (en) | 1997-04-03 | 1999-06-11 | Hispano Suiza Sa | DEVICE FOR CLOSING AND LOCKING THE SHUTTERS OF A PUSH INVERTER |
US6021636A (en) * | 1997-07-25 | 2000-02-08 | Alliedsignal Inc. | Lightweight tertiary thrust reverser lock assembly with a blocking member |
GB9907614D0 (en) * | 1999-04-06 | 1999-05-26 | Lucas Ind Plc | Lock for a thrust reverser |
FR2823258B1 (en) * | 2001-04-05 | 2003-09-19 | Hispano Suiza Sa | EMERGENCY LOCKING SYSTEM FOR PUSH INVERTER DOOR |
FR2823259B1 (en) * | 2001-04-05 | 2003-06-27 | Hispano Suiza Sa | SYNCHRONIZED LOCKING SYSTEM FOR THE DOORS OF A PUSH INVERTER |
US6604355B1 (en) * | 2001-08-31 | 2003-08-12 | The Boeing Company | Thrust reverser hook latch system |
US6568172B2 (en) | 2001-09-27 | 2003-05-27 | The Nordam Group, Inc. | Converging nozzle thrust reverser |
BR0315201A (en) | 2002-10-11 | 2005-08-16 | Nordam Group Inc | Double Fold Boost Inverter |
-
2004
- 2004-08-30 US US10/929,809 patent/US7146796B2/en active Active
- 2004-08-31 EP EP04816835A patent/EP1676025B1/en active Active
- 2004-08-31 CA CA2536693A patent/CA2536693C/en not_active Expired - Fee Related
- 2004-08-31 WO PCT/US2004/028255 patent/WO2005040589A2/en active Application Filing
- 2004-08-31 BR BRPI0414047A patent/BRPI0414047B1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
BRPI0414047B1 (en) | 2019-08-27 |
CA2536693C (en) | 2013-03-12 |
WO2005040589A3 (en) | 2006-02-16 |
US7146796B2 (en) | 2006-12-12 |
CA2536693A1 (en) | 2005-05-06 |
EP1676025A2 (en) | 2006-07-05 |
EP1676025B1 (en) | 2012-11-14 |
WO2005040589A2 (en) | 2005-05-06 |
EP1676025A4 (en) | 2010-04-14 |
US20050102996A1 (en) | 2005-05-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25G | Requested change of headquarter approved |
Owner name: THE NORDAM GROUP, INC. (US) |
|
B07A | Application suspended after technical examination (opinion) [chapter 7.1 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 10 (DEZ) ANOS CONTADOS A PARTIR DE 27/08/2019, OBSERVADAS AS CONDICOES LEGAIS. (CO) 10 (DEZ) ANOS CONTADOS A PARTIR DE 27/08/2019, OBSERVADAS AS CONDICOES LEGAIS |
|
B21F | Lapse acc. art. 78, item iv - on non-payment of the annual fees in time |
Free format text: REFERENTE A 17A ANUIDADE. |
|
B24J | Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12) |
Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2635 DE 06-07-2021 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013. |